# Service difficulty reports: Lockheed 188C

A list on [Lockheed 188C](https://openairdocs.org/model/lockheed-188c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 15 · 732 reports

- [SDR CA190624019](https://openairdocs.org/sdr/CA190624019.md): Landing Gear · binding · Jun 22, 2019 · Lkheed 188C · Landing Gear Retraction/Extension System
  > (CAN) GEAR WAS SELECTED UP AND LEFT MAIN GEAR LIGHT REMAINED IN UNSAFE INDICATION. TRIED RECYCLING GEAR SEVERAL TIMES WITH NO LUCK, VISUALLY CONFIRMED GEAR WAS JAMMED IN A PARTIALLY UP POSITION. AIRCRAFT LANDED GEAR UP (TC# 20190624019)
- [SDR CA150703011](https://openairdocs.org/sdr/CA150703011.md): Engine · power loss · Jul 1, 2015 · Lkheed 188C · Engine (Turbine/Turboprop)
  > (CAN) UPON COMPLETION OF BOMB RUN (AIRCRAFT WAS PERFORMING FIRE SUPPRESSION ACTIVITIES), CLIMB OUT WAS INITIATED. THE AIRCRAFT PASSED THROUGH AN ERUPTION IN THE FIRE CAUSING THE AIRCRAFT TO YAW CONSIDERABLE TO THE LEFT, BOTH THE NR 1 AND 2 ENGINES OVER TEMP WA
- [SDR CA150519030](https://openairdocs.org/sdr/CA150519030.md): Fitting · cracked · May 15, 2015 · Lkheed 188C · Turbine Engine Oil System
  > (CAN) LOST OIL PRESSURE IN NR 3 ENGINE ON TAXI AFTER LANDING. MAINTENANCE NOTED CRACK AT RGB OIL PRESSURE INLET FITTING, DEFECTIVE ENGINE WAS REMOVED FOR FURTHER INVESTIGATION, SERVICEABLE ENGINE INSTALLED, ACFT RETURNED TO SERVICE.
- [SDR CA150514003](https://openairdocs.org/sdr/CA150514003.md): Wire · broken · May 12, 2015 · Lkheed 188C · Engine Oil System Wiring
  > (CAN) DURING CLIMB AND CRUISE, THE FLIGHT CREW NOTED THE NR 4 ENGINE OIL QTY WAS LOW, INDICATING TWO GALLONS, A LOSS OF SIX GALLONS. NO SIGN OF FLUID LEAK WAS NOTED BUT A PRECAUTIONARY SHUTDOWN OF THE AFFECTED ENGINE WAS CARRIED OUT. DISCOVERED & REPAIRED A
- [SDR CA150406006](https://openairdocs.org/sdr/CA150406006.md): Tube · cracked · Apr 2, 2015 · Lkheed 188C · Hydraulic System, Main
  > (CAN) DURING TRAINING FLIGHT, BALKED APPROACH AND AFTER COMPLETING THE CLIMB CHECKLIST, IT WAS NOTED THAT THE HYD FLUID QTY IN HYD SYS 1 WAS VERY LOW. THE SYSTEM WAS SHUTDOWN IAW HYD SYSTEM MALFUNCTION, LOSS OF HYD FLUID CHECKLIST. IMMEDIATE RETURN FOR LANDI
- [SDR CA140630026](https://openairdocs.org/sdr/CA140630026.md): Reduction Gb · making metal · Jun 30, 2014 · Lkheed 188C · Turbine Engine Reduction Gear
  > (CAN) INCREASED CONSUMPTION OF OIL, LEAD TO INSPECTION OF RGB OIL SCREEN WHERE METAL PARTICLES WERE FOUND. ENGINE REMOVED FROM SERVICE.
- [SDR CA140613005](https://openairdocs.org/sdr/CA140613005.md): Tach Generator · malfunctioned · Jun 2, 2014 · Lkheed 188C · Engine RPM Indicating System
  > (CAN) ON FIRE ACTION, NOTICED THE NR 2 ERPM GAUGE HAD BACKED OFF TO 13200 RPM. TIT, HP, FF AND HERTZ ALL READ NORMAL. THE MEL REQUIRES 4 ENGINE TACHOMETERS FUNCTIONING, ELECTED TO SHUTDOWN ENGINE 2 IAW SOP. SECURED ENGINE, COMPLETED ABNORMAL PREAMBLE AND 1 E
- [SDR CA140613007](https://openairdocs.org/sdr/CA140613007.md): Pump · failed · May 9, 2014 · Lkheed 188C · Hydraulic Pump (Electric/Engine), Main
  > (CAN) NR 1 HYDRAULIC SYS OVERHEAT LIGHT CAME ON IN FLIGHT COINCIDING WITH FAILED GENERATOR SDR 20140613006.
- [SDR CA140613006](https://openairdocs.org/sdr/CA140613006.md): Generator · failed · May 8, 2014 · Lkheed 188C · AC Generator-Alternator
  > (CAN) NR 3 GENERATOR TRIPPED, UNDER-SPEED, TWICE, LT OFF. TEAR DOWN REPORT.
- [SDR CA120917016](https://openairdocs.org/sdr/CA120917016.md): Engine · power loss · Sep 13, 2012 · Lkheed 188C · Engine (Turbine/Turboprop)
  > (CAN) SECURED NR 1 ENGINE DURING CLIMBOUT. DURING CLIMBOUT, FLIGHT CREW HEARD A, POP/BANG. SCANNED ENGINE INSTRUMENTS AND NOTICED LOSS OF HORSEPOWER AND DECAYING RPM ON NR 1 ENGINE. E-HANDLED NR 1 ENGINE TO SHUTDOWN AND FEATHER PROPELLER. ABORTED THE LOAD
- [SDR CA120716012](https://openairdocs.org/sdr/CA120716012.md): Fuel Control · malfunctioned · Jul 12, 2012 · Lkheed 188C · Engine (Turbine/Turboprop)
  > (CAN) DURING CLIMB-OUT PHASE OF BOMBING RUN, WITH POWER LEVERS ADVANCED. CREW NOTICED HIGH TIT, LOW TORQUE AND ERRATIC RPM ON THE NR 2 ENGINE. AN ENGINE SHUTDOWN WAS EXECUTED AND THE ACFT RETURNED TO BASE. ACFT WAS 3 ENGINE FERRIED BACK TO HOME THE FOLLOWING
- [SDR CA120712001](https://openairdocs.org/sdr/CA120712001.md): Solenoid Valve · failed · Jul 7, 2012 · Lkheed 188C · Propeller Controlling System
  > (CAN) WHILE ADVANCING POWER LEVER ON CLIMB OUT ENGINE TORQUE WAS UN-RESPONSIVE. THIS WAS CAUSE BY A FAULTY PROPELLER GOVERNING SYS THAT CAUSED THE ENGINE RPM TO CLIMB UNTIL THE FCU OVERSPEED GOVERNOR SETTING WAS REACHED PRIOR TO THE FINAL POWER LEVER ADVANCEM
- [SDR CA120404003](https://openairdocs.org/sdr/CA120404003.md): Switch · failed · Mar 31, 2012 · Lkheed 188C · Landing Gear Retraction/Extension System
  > (CAN) THE SNAG WAS REPORTED AS HAD A IN TRANSIT, UNSAFE GEAR LIGHT ON THE NLG AND LT MLG AFTER 45 SECONDS, BUMPED UP GEAR HANDLE UP TO ENSURE POSITIVE SELECTION, THEN WENT TO NEUTRAL, GEAR STAYED UP, WENT TO GEAR DOWN, GEAR CAME DOWN, 3 GREEN RETURNED TO BS TO
- [SDR CA111115010](https://openairdocs.org/sdr/CA111115010.md): Actuator · damaged · Nov 15, 2011 · Lkheed 188C · Rudder Actuator
  > (CAN) TANKER 484 HAD AN EXTERNALLY LEAKING RUDDER ACTUATOR. ON DIS-ASSEMBLY IT WAS DISCOVERED THAT THE PLUGS SERVING AS STOPS FOR A CYLINDER DIVIDER ASSEMBLY WERE BROKEN OFF. THIS COLLAR SERVED TO HOUSE O RINGS & SEPARATE HYD PRESSURES FROM SYSTEMS 1 & 2. B
- [SDR CA110714001](https://openairdocs.org/sdr/CA110714001.md): Engine · malfunctioned · Jul 12, 2011 · Lkheed 188C · Engine (Turbine/Turboprop)
  > (CAN) TAXIING TO TANKER BASE AFTER LANDING. ENGINE SHIFT-DOWN WAS SELECTED MOMENTARILY BY AIRCREW, HOWEVER ENGINE SPEED SOLENOID SWITCH WAS NOT GIVEN TIME TO LATCH. ENGINE RPM HAD SPOOLED DOWN TO "LOW" AND THEN IMMEDIATELY SPOOLED BACK UP. AIRCREW NOTICED A
- [SDR CA090824011](https://openairdocs.org/sdr/CA090824011.md): Brush Block · worn · Aug 24, 2009 · Lkheed 188C · Propeller Controlling System
  > ON RETURN NR4 ENG RPM DROOPED TO 13,600. WHILE REVIEWING CHECKLIST FOR POSSIBLE ENG SHUTDOWN, ENG DROOPED TO 13,450 AND BEGAN TO HAVE HORSEPOWER SURGES. ENG WAS SHUTDOWN AND SECURED. IAW SOP’S (PROP GOVERNOR WAS CHANGED AND ACFT GROUND RUN AND RETURNED TO SER
- [SDR CA090727011](https://openairdocs.org/sdr/CA090727011.md): Linkage · out of rig · Jul 25, 2009 · Lkheed 188C · Propeller Feathering/Reversing
  > LOCAL TEST FLIGHT. ENGINE SHUTDOWNS AND RESTARTS PERFORMED. NR 1 ENG DEVELOPED A RPM FLUCTUATION. WANDERING 4-500 RPM. ENGINE MONITORED. SEVERAL CHECKS PERFORMED. ENGINE SHUTDOWN AND SECURED IAW COMPANY SOP. ENGINE INOP PROCEDURES FOLLOWED. UNEVENTFUL LA
- [SDR CA090615008](https://openairdocs.org/sdr/CA090615008.md): Engine · fluctuates · Jun 12, 2009 · Lkheed 188C · Engine (Turbine/Turboprop)
  > (CAN) NUMBER ONE ENGINE TIT WAS FLUCTUATING BETWEEN 750-830 DEG. THE HORSEPOWER WAS ALSO FLUCTUATING THE RPM WAS STABLE. AS A PRE-CAUTIONARY THE CREW ELECTED TO SHUT NUMBER ONE ENGINE DOWN, THE ABNORMAL CONFIGURATION CHECK LIST WAS CARRIED OUT AND ONE ENGINE I
- [SDR CA070730005](https://openairdocs.org/sdr/CA070730005.md): Structure · separated · Jul 28, 2007 · Lkheed 188C · Trailing Edge Flaps
  > (CAN) FIRE SUPPRESSION OPERATIONS IN RUGGED MOUNTAINOUS TERRAIN. FINISHED LAST OF 4 DROPS. APPLIED MAX POWER AND FLAPS TO 78 PERCENT AND PROCEEDED WITH CLEAN UP CHECKLIST. NOTICED ABNORMAL OF CONTROL COLUMN ( MORE AILERON). ADJUSTED TRIMS AND POWER SETTINGS.
- [SDR CA070715001](https://openairdocs.org/sdr/CA070715001.md): Fitting · leaking · Jul 14, 2007 · Lkheed 188C · Turbine Engine Oil System
  > (CAN) THE CREW NOTICED A LOSS OF OIL QUANTITY ON THE NR 3 ENGINE. THIS LOSS WAS FOLLOWED BY A FLUCTUATION IN THE REDUCTION GEARBOX PRESSURE. THE ENGINE WAS SHUTDOWN PRIOR TO LANDING. IT WAS DETERMININED THAT A FITTING ON THE TURBINE SECTION WAS LEAKING. THERE
- [SDR CA060412002](https://openairdocs.org/sdr/CA060412002.md): Line · missing · Apr 11, 2006 · Lkheed 188C · Engine Fuel and Control
  > (CAN) NR 2 ENGINE HAD A HUNG RESTART WHILE ON A TRAINING FLIGHT, THE ENGINE WAS SHUTDOWN, SECURED AND THE (3) ENGINE PROCEDURES WHEN FOLLOWED ON THE FLIGHT AND LANDING TO THE MAINTENANCE BASE. THE PRIMER PRESSURE LINE WAS FOUND TO BE NOT INSTALLED ON THIS ENGI
- [SDR CA050613003](https://openairdocs.org/sdr/CA050613003.md): Governor · malfunctioned · Jun 10, 2005 · Lkheed 188C · Propeller Governor
  > (CAN) ON DESCEND TO A BOMBING RUN RPM AND FUEL FLOW WERE HIGH ON NR 4 ENGINE. THE ENGINE WAS SHUT DOWN AND FEATHERED, THE A/C RETURNED WITH OUT INCEDENT TO HIGH LEVEL A IRPORT. THE PROP GOVENOR WAS AJUSTED ANDTHE A/C WAS RETURED TO SERVICE.
- [SDR CA050530007](https://openairdocs.org/sdr/CA050530007.md): Mount · failed · May 27, 2005 · Lkheed 188C · Fuel Control/Turbine Engines
  > (CAN) ON LANDING ROLL OUT THE NR 1 ENGINE FIREBELL WENT OFF, THE CREW HANDLED THE ENGINE AND THE FIRE BELL WENT OUT. MAINTENANCE FOUND THE AFT SECTION OF THE REAR BEARING SUPPORT AND SWIRL STRAIGHTENER IN THE EXHAUST BELL HOUSING PIPE. THERE WAS SOME COWL DA
- [SDR CA050418014](https://openairdocs.org/sdr/CA050418014.md): Rotary Actuator · failed · Apr 18, 2005 · Lkheed 188C · Propeller Governor
  > (CAN) AT EIGHT THOUSAND FEET WHILE SLOWING THROUGH 160 KTS, ON THE TC CHECK RIDE, NR 3 PROP OVERSPEED TO 14,550 ERPM. THE ENGINE WAS SHUT DOWN AND PROP FEATHERED. THE A/C RETURNED TO CYQF AND LANDED WITHOUT INCIDENTS. MAINTENANCE FOUND ROTARY ACTUATOR DRIVE
- [SDR CA041105005](https://openairdocs.org/sdr/CA041105005.md): Fuel Control · failed · Nov 5, 2004 · Lkheed 188C · Fuel Controlling System
  > (CAN) ON TEST FLIGHT A/C WAS WEST OF OF THE AIRFIELD IN THE PRACTICE AREA. NR 3 ENGINE WAS SHUTDOWN AND SECURED DUE TO LACK OF RESPONSE WITH THE POWER LEVER. THE A/C RETURNED TO BASE WITHOUT INCIDENT. FCU IS SUSPECTED.
- [SDR ZIAA04059](https://openairdocs.org/sdr/ZIAA04059.md): Floor Support · corroded · Dec 8, 2003 · N286F · Lkheed 188C · Fuselage Miscellaneous Structure
  > YIP - FOUND RIGHT WING CENTER SECTION RBL 40 AT NR 1 PLANK UPPER SURFACE CORROSION AT FLOOR SUPPORT BRACKET. REMOVED CORROSION AND TREATED AREA PER L-188 SRM 51-2-14. MATERIAL REMOVED IS PAST NEGLIGIBLE LIMITS. REPAIRED AREA PER L-188 SRM 57-2-1, PAGE 19. R
- [SDR ZIAA04058](https://openairdocs.org/sdr/ZIAA04058.md): Door Frame · cracked · Sep 20, 2002 · N286F · Lkheed 188C · Fuselage Main, Structure
  > YIP - INVESTIGATE X-RAY INDICATIONS AT 2 RIVETS MARKED IN RED ON OUTER SURFACE OF AFT LOWER CARGO DOOR, LOWER FORWARD CORNER. REMOVED REPAIR DOUBLERS TO INVESTIGATE FUSELAGE SKIN. FOUND EXISTING CRACK WAS STOP DRILLED PER L-188 SRM 53-2-1, FIG 2, SHEET 6. R
- [SDR ZIAA04057](https://openairdocs.org/sdr/ZIAA04057.md): Skin · corroded · Nov 27, 2001 · N286F · Lkheed 188C · Wing, Plate/Skin
  > YIP - REMOVE REPAIR INSTALLATION AT RT WING UPPER SURFACE, WS 70, 7/8 PLANK SEAM FOR CO CONVENIENCE. CONFIRM THE EXTENT OF DAMAGE AT THIS LOCATION. INSTALL REPAIR PER ZANTOP DWG A72-R03. REMOVED EXTERNAL DOUBLERS ON PLANK 7/8 SEAM AT WS 65-83. CONFIRM CORR
- [SDR ZIAA04050](https://openairdocs.org/sdr/ZIAA04050.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame
  > FOUND FUSELAGE FRAME CRACKED AT FS 716 AT STRINGER 72. REPAIRED FRAME AT STRINGER 68-1 PER L-188 SRM 53-2-3, FIG 2. (M)
- [SDR ZIAA04049](https://openairdocs.org/sdr/ZIAA04049.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame
  > YIP - FOUND FUSELAGE FRAME CRACKED AT FS 654 BETWEEN STRINGER 9-10. REPAIRED FRAME AT STRINGER 9-10 IAW L-188 SRM 53-2-3, FIG 2. (M)
- [SDR ZIAA04056](https://openairdocs.org/sdr/ZIAA04056.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame
  > FOUND FUSELAGE FRAME CRACKED AT FS 654 STRINGER 13. REPAIRED FRAME AT STRINGER 13 PER L-188 SRM 53-2-3, FIG 2. (M)
- [SDR ZIAA04043](https://openairdocs.org/sdr/ZIAA04043.md): Floorbeam · corroded · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Floor Beam
  > YIP - FOUND FLOORBEAM AT FS 200 RIGHT SIDE NEAR PORTA POTTY AREA CORRODED. REMVOED CORRODED SECTION OF FLOORBEAM AND REPAIRED FS 200 FLOORBEAM PER L-188 SRM 53-2-4, FIG 2 SHEET 1. (M)
- [SDR ZIAA04055](https://openairdocs.org/sdr/ZIAA04055.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame
  > FOUND FUSELAGE FRAME CRACKED AT FS 397.5, STRINGER 21. REPAIRED FRAME IAW L-188 SRM 53-2-3, FIG 2. (M)
- [SDR ZIAA04054](https://openairdocs.org/sdr/ZIAA04054.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame
  > YIP - FOUND FUSELAGE FRAME CRACKED AT FS 401, STRINGER 8. REPAIRED FRAME AT STRINGER 8 PER L-188 SRM 53-2-3 FIG 2. (M)
- [SDR ZIAA04042](https://openairdocs.org/sdr/ZIAA04042.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame
  > FOUND FUSELAGE FRAME CRACKED AT FS 407 BETWEEN STRINGERS 1-2. REPAIRED FRAME AT STRINGER 1-2 PER L188 SRM 53-2-3, FIG 2. (M)
- [SDR ZIAA04041](https://openairdocs.org/sdr/ZIAA04041.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame
  > YIP - FOUND FUSELAGE FRAME CRACKED AT FS 388 BETWEEN STRINGERS 72-1. REPAIRED FRAME AT STRINGER 72-1 PER LOCKHEED S/B 706 DWG 842354. (M)
- [SDR ZIAA04053](https://openairdocs.org/sdr/ZIAA04053.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame
  > YIP - FOUND FUSELAGE FRAME CRACKED AT FS 407, STRINGER 8. REPAIRED FRAME AT STRINGER 8 PER L-188 SRM 53-2-3, FIG 2. (M)
- [SDR ZIAA04048](https://openairdocs.org/sdr/ZIAA04048.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame
  > YIP - FOUND FUSELAGE FRAME CRACKED AT FS 578 BETWEEN STRINGERS 72-1. REPAIRED FRAME AT STRINGER 72-1 IAW L-188 SRM 53-2-3 FIG 2. (M)
- [SDR ZIAA04047](https://openairdocs.org/sdr/ZIAA04047.md): Frame · corroded · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame
  > FOUND LIGHT CORROSION ON FRAME AT FS 540 STRINGER 69. REMOVED CORROSION AND REPAIRED FRAME PER L-188 SRM 53-2-3, FIG 2. PLUGGED NEGLIBIBLE HOLES PER L-188 SRM 51-3-6, FIG 1. (M)
- [SDR ZIAA04046](https://openairdocs.org/sdr/ZIAA04046.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame
  > YIP - FOUND FUSELAGE FRAME CRACKED AT FS 464 AT STRINGER 70-71. REPAIRED FRAME AT STRINGER 70-71 IAW L-188 SRM 53-2-3, FIG 2. (M)
- [SDR ZIAA04045](https://openairdocs.org/sdr/ZIAA04045.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame
  > YIP - FOUND FUSELAGE FRAME CRACKED AT FS 426 AT STRINGER 71. REPAIRED FRAME AT FS 426 FROM STRINGER 68-4 IAW L-188 SRM 53-2-3. (M)
- [SDR ZIAA04051](https://openairdocs.org/sdr/ZIAA04051.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame
  > YIP - FOUND FUSELAGE FRAME CRACKED AT FS 730, STRINGER 72. REPAIRED FRAME AT STRINGER 72 PER L-188 S/B 706 DWG 842354. (M)
- [SDR ZIAA04052](https://openairdocs.org/sdr/ZIAA04052.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame
  > FOUND FUSELAGE FRAME CRACKED AT FS 920 BETWEEN STRINGERS 67-69. REPAIRED FRAME AT STRINGER 66-69 PER L-188 SRM 53-2-3, FIG 2. (M)
- [SDR ZIAA04044](https://openairdocs.org/sdr/ZIAA04044.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame
  > FOUND FUSELAGE FRAME CRACKED AT FS 426 AT STRINGER 1. REPAIRED FRAME AT FS 426 FROM STRINGER 68-4 IAW L-188 SRM 53-2-3. (M)
- [SDR ZIAA04001](https://openairdocs.org/sdr/ZIAA04001.md): Doubler · cracked · Jul 30, 2001 · N286F · Lkheed 188C · Wing, Plate/Skin
  > FOUND WS 249 LOWER SURFACE, LEAP DOUBLER AT FORWARD EDGE IS CRACKED AT RIGHT WING. ROUTED OUT DEFECTIVE AREA OF LEAP DOUBLER. DYE PEN OF WING PLANK REVEALED NO DISCREPANCIES. REPAIRED IAW L188 SRM 57-2-1 AND SEALED INTERNALLY. (M)
- [SDR ZIAA04003](https://openairdocs.org/sdr/ZIAA04003.md): Doubler · cracked · Jul 30, 2001 · N286F · Lkheed 188C · Wing, Plate/Skin
  > FOUND LOWER SURFACE AT WS 265 RIGHT WING LEAP DOUBLER ON PLANK NR 4 IS CRACKED. LEAK CHECK DUE. ROUTED OUT CRACKED LEAP DOUBLER MATERIAL. INSPECTED WING PLANK SURFACE WITH DYE PEN. NO DEFECTS FOUND. REPAIRED PER L-188 SRM 57-2-1, FIG 3, SHEET 30, TYPE 2.
- [SDR ZIAA04002](https://openairdocs.org/sdr/ZIAA04002.md): Doubler · cracked · Jul 30, 2001 · N286F · Lkheed 188C · Wing, Plate/Skin
  > YIP - FOUND LWER SURFACE AT WS 253, FORWARD EDGE OF LEAP DOUBLER IS CRACKED, RIGHT WING. CRACK STOP DRILLED, ROUTED OUT DEFECTIVE AREA OF LEAP DOUBELR. DYE PEN OF WING PLANK REVEALED NO DISCREPANCIES. REPAIRED IAW L-188 SRM 57-2-1 AND SEALED INTERNALLY. (M
- [SDR RAAA01E406](https://openairdocs.org/sdr/RAAA01E406.md): Frame · bent · Apr 11, 2001 · N9744C · Lkheed 188C · Fuselage Main, Frame
  > DURING SCHEDULED #4 MAINTENANCE CHECK, FOUND FORMER BENT IN BETWEEN STR 36 & 39. REPAIRED FORMER PER L-188 SRM 53-2-3.
- [SDR RAAA01E405](https://openairdocs.org/sdr/RAAA01E405.md): Frame · bent · Apr 11, 2001 · N9744C · Lkheed 188C · Fuselage Main, Frame
  > DURING SCHEDULED NR 4 MAINTENANCE CHECK, FOUND FORMER BENT IN BETWEEN STR 34 & 36. REPAIRED FORMER PER SRM 53-2-3.
- [SDR RAAAO1E404](https://openairdocs.org/sdr/RAAAO1E404.md): Skin · torn · Apr 11, 2001 · N9744C · Lkheed 188C · Cargo/Baggage Doors
  > DURING SCHEDULED NR 4 MAINTENANCE CHECK, FOUND FWD BAGGAGE PIT DOOR SKIN TORN AT LOWER AFT EDGE. REPAIRED PER L-188 SRM 53-2-1 FIG 2. M-54 # 162

Next page: https://openairdocs.org/model/lockheed-188c/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = '188C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/lockheed-188c/reports

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